A review of computational aeroelasticity of civil fan blades

M Vahdati, KB Lee, P Sureshkumar - International Journal of Gas …, 2020 - jstage.jst.go.jp
This paper presents a review of aeroelasticity research concerning fan blades in modern
civil aircraft engines. It summarises the research carried out at the Rolls-Royce Vibration …

A review on theoretical and numerical research of axial compressor surge

H Zhao, J Du, W Zhang, H Zhang, C Nie - Journal of Thermal Science, 2023 - Springer
Surge is an unstable operating condition of the aero-engine that can move the engine into a
destabilized state and cause devastating damage. One of the most popular topics in the …

Application of artificial intelligence in turbomachinery aerodynamics: Progresses and challenges

Z Zou, P Xu, Y Chen, L Yao, C Fu - Artificial Intelligence Review, 2024 - Springer
Turbomachinery plays a vital role in energy conversion systems, with aerodynamic issues
being integral to its entire lifecycle, spanning the period of design, validation, and …

Investigation of hemocompatibility and vortical structures for a centrifugal blood pump based on large-eddy simulation

Y Liu, N Xie, Y Tang, Y Zhang - Physics of Fluids, 2022 - pubs.aip.org
The evolution of complex flow structures has a large impact on the hemocompatibility of the
centrifugal blood pump. In this study, the hemodynamic performance and the …

Influence of the inlet distortion on fan stall margin at different rotational speeds

W Zhang, S Stapelfeldt, M Vahdati - Aerospace Science and Technology, 2020 - Elsevier
The aim of this paper is to develop a reliable and accurate numerical strategy that can be
used to study the effects of inlet distortions on the aerodynamic stability of fan blades in aero …

Comparison of DDES and URANS for unsteady tip leakage flow in an axial compressor rotor

Y Liu, L Zhong, L Lu - Journal of Fluids Engineering, 2019 - asmedigitalcollection.asme.org
Tip leakage vortex (TLV) has a large impact on compressor performance and should be
accurately predicted by computational fluid dynamics (CFD) methods. New approaches of …

Uhbr open-test-case fan ecl5/catana

V Pagès, P Duquesne, S Aubert, L Blanc… - International Journal of …, 2022 - mdpi.com
The application of composite fans enables disruptive design possibilities but increases
sensitivity to multi-physical resonance between aerodynamic, structure dynamic and …

Numerical investigation of corner separation flow using Spalart-Allmaras model with various modifications

W Li, Y Liu - Aerospace Science and Technology, 2022 - Elsevier
Three-dimensional corner separation is an inherent flow feature in axial compressors which
blocks flow path and worsens the performance. To find an effective turbulence model for …

Passive separation control with blade-end slots in a highly loaded compressor cascade

Y Tang, Y Liu, L Lu, H Lu, M Wang - AIAA Journal, 2020 - arc.aiaa.org
The proposed passive control method, blade-end slots, is implemented to reorganize the
blade-end flow in a highly loaded compressor cascade under a wide incidence range at M …

Extending highly loaded axial fan operability range through novel blade design

DI Lopez, T Ghisu, T Kipouros… - Journal of …, 2022 - asmedigitalcollection.asme.org
The tip clearance size has historically been considered to be the main factor affecting
stability range in axial fan and compressors. This paper reveals that the stall characteristics …